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APPARATUS AND METHODS FOR SEALING COMPONENTS IN GAS TURBINE ENGINES

  • US 20160245108A1
  • Filed: 02/22/2016
  • Published: 08/25/2016
  • Est. Priority Date: 02/20/2015
  • Status: Active Application
First Claim
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1. An apparatus adapted for use in a gas turbine engine, the apparatus comprisinga first circumferential member, an end portion of the first circumferential member defining a recess and including a first seal surface;

  • anda second circumferential member, an end portion of the second circumferential member configured to be at least partially disposed within the recess of the first circumferential member, the end portion of the second circumferential member including a second seal surface,the first circumferential member and the second circumferential forming at least a portion of a circumferential assembly of a gas turbine when the end portion of the second circumferential member is at least partially disposed within the recess of the first circumferential member, the first seal surface configured to form a first seal with a seal member and the second seal surface configured to form a second seal with the seal member when the end portion of the second circumferential member is at least partially disposed within the recess of the first circumferential member.

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